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Evolution of Artificial Perturbations in the Boundary Layer on a Plate and in Its Wake at Supersonic Free-Stream Velocity |
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| Authors: | Yu. G. Ermolaev V. I. Lysenko |
| Abstract: | The evolution of artificial perturbations in the boundary layer on the flat section of a plate, on the backward-facing wedge behind the rarefaction wave fan, and in the wake is studied experimentally at the Mach number M =2. |
| Keywords: | boundary layer supersonic flow rarefaction waves plate backward-facing wedge wake |
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